This chapter discusses the physics of classical flutter and then shows how to practically determine the conditions that lead to instability. The root locus procedure is also presented. Additional methods to find the flutter speed (such as the \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$p-k$$\end{document} and g methods) will be covered in Chap. 36.
Classical Flutter, State-Space Model, and Root Locus
Introduction to Unsteady Aerodynamics and Dynamic Aeroelasticity ; Kapitel : 35 ; 609-621
2024-06-11
13 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
A root locus-based flutter synthesis procedure
NTRS | 1983
|A root locus based flutter synthesis procedure
AIAA | 1983
|A root locus-based flutter synthesis procedure
AIAA | 1983
|TIBKAT | 1962
|State-space formulations for flutter analysis
AIAA | 1977
|